Invention Grant
- Patent Title: Jet engine exhaust nozzle flow effector
- Patent Title (中): 喷气发动机排气喷嘴流量计
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Application No.: US11762827Application Date: 2007-06-14
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Publication No.: US07958733B2Publication Date: 2011-06-14
- Inventor: Travis L. Turner , Roberto J. Cano , Richard J. Silcox , Ralph D. Buehrle , Christopher M. Cagle , Randolph H. Cabell , George C. Hilton
- Applicant: Travis L. Turner , Roberto J. Cano , Richard J. Silcox , Ralph D. Buehrle , Christopher M. Cagle , Randolph H. Cabell , George C. Hilton
- Applicant Address: US DC Washington
- Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Current Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Current Assignee Address: US DC Washington
- Agent Andrea Z. Warmbier; Helen M. Galus; Barry V. Gibbens
- Main IPC: F02K1/00
- IPC: F02K1/00
Abstract:
A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.
Public/Granted literature
- US20080272232A1 Jet Engine Exhaust Nozzle Flow Effector Public/Granted day:2008-11-06
Information query
